The invention discloses a refueling manifold system and an aircraft pressure refueling assembly with the same and an aircraft. The refueling manifold system comprises a refueling manifold (1), a refueling branch (3), an emergency defueling branch (4) and a check valve (5), wherein the refueling manifold (1) penetrates through a fuel tank (2), the refueling manifold (1) enters the fuel tank (2) from a first wallboard (21) of the fuel tank (2), and extends out of the fuel tank (2) from a second wallboard (22) of the fuel tank (2); the refueling branch (3) is arranged at a position, located in the fuel tank, of the refueling manifold (1); the check valve (5) is arranged at a position, located in the fuel tank, of the refueling manifold (1), and adjacent to the first wallboard (21). The check valve of the refueling manifold (1) of the refueling manifold system disclosed by the invention is arranged at a position, located in the fuel tank, of the refueling manifold and adjacent to the first wallboard, so that fuel in a pipeline in front of the check valve can be completed discharged.


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    Titel :

    Refueling manifold system and aircraft pressure refueling assembly with same and aircraft


    Beteiligte:
    YU GUOJI (Autor:in) / LIN HOUYAN (Autor:in) / MA SHAOPU (Autor:in)

    Erscheinungsdatum :

    2016-02-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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